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In this paper, the modeling and robust control design of a vertical flight attitude control for a mini tail-sitter with variable pitch propeller is discussed. Tail-sitters vertical take-off and landing - unmanned aerial vehicles (VTOL-UAVs) have the operational flexibility of a typical helicopter while having the cruise performance of a fixed wing airplanes. The VTOL-UAVs configuration used in this...
In this paper, the modeling and control design of a vertical flight attitude control for a mini tail-sitter with variable pitch propeller is discussed. Tail-sitters VTOL-UAVs have operational flexibility of typical helicopters while having the cruise performance of fixed wing airplanes. The configuration proposed in this work is highly unstable in its natural flight state in vertical mode. A dynamic...
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